diff options
| author | Roman Bapst <romanbapst@yahoo.de> | 2015-01-19 09:56:42 +0100 |
|---|---|---|
| committer | Lorenz Meier <lm@inf.ethz.ch> | 2015-01-20 13:01:41 +0100 |
| commit | 70c7764b9f9e780664ae13d0962a55dd226117e6 (patch) | |
| tree | 55a08b56341e8c0cdd1ea8b1077d4620ae51d24a /src/modules/uORB/topics | |
| parent | f3dcde39935766626155be70a88a89f4962af30a (diff) | |
| download | px4-firmware-70c7764b9f9e780664ae13d0962a55dd226117e6.tar.gz px4-firmware-70c7764b9f9e780664ae13d0962a55dd226117e6.tar.bz2 px4-firmware-70c7764b9f9e780664ae13d0962a55dd226117e6.zip | |
removed secondary attitude from attitude topic
Diffstat (limited to 'src/modules/uORB/topics')
| -rwxr-xr-x | src/modules/uORB/topics/vehicle_attitude.h | 18 |
1 files changed, 0 insertions, 18 deletions
diff --git a/src/modules/uORB/topics/vehicle_attitude.h b/src/modules/uORB/topics/vehicle_attitude.h index 77324415a..019944dc0 100755 --- a/src/modules/uORB/topics/vehicle_attitude.h +++ b/src/modules/uORB/topics/vehicle_attitude.h @@ -79,24 +79,6 @@ struct vehicle_attitude_s { float g_comp[3]; /**< Compensated gravity vector */ bool R_valid; /**< Rotation matrix valid */ bool q_valid; /**< Quaternion valid */ - - // secondary attitude, use for VTOL - float roll_sec; /**< Roll angle (rad, Tait-Bryan, NED) */ - float pitch_sec; /**< Pitch angle (rad, Tait-Bryan, NED) */ - float yaw_sec; /**< Yaw angle (rad, Tait-Bryan, NED) */ - float rollspeed_sec; /**< Roll angular speed (rad/s, Tait-Bryan, NED) */ - float pitchspeed_sec; /**< Pitch angular speed (rad/s, Tait-Bryan, NED) */ - float yawspeed_sec; /**< Yaw angular speed (rad/s, Tait-Bryan, NED) */ - float rollacc_sec; /**< Roll angular accelration (rad/s, Tait-Bryan, NED) */ - float pitchacc_sec; /**< Pitch angular acceleration (rad/s, Tait-Bryan, NED) */ - float yawacc_sec; /**< Yaw angular acceleration (rad/s, Tait-Bryan, NED) */ - float rate_offsets_sec[3]; /**< Offsets of the body angular rates from zero */ - float R_sec[3][3]; /**< Rotation matrix body to world, (Tait-Bryan, NED) */ - float q_sec[4]; /**< Quaternion (NED) */ - float g_comp_sec[3]; /**< Compensated gravity vector */ - bool R_valid_sec; /**< Rotation matrix valid */ - bool q_valid_sec; /**< Quaternion valid */ - }; /** |